View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 62427U 26145.54178846 +.00000000 +00000-0 +64735-3 0 00003
2 62427 42.9983 240.3619 0000510 257.2283 102.8512 15.27596295 08
| Epoch (UTC): | 25 May 2026 13:00:10 |
| Eccentricity: | 0.0000510 |
| inclination: | 42.9983° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 240.3619° |
| argument of perigee: | 257.2283° |
| revolutions per day: | 15.27596295 |
| mean anomaly at epoch: | 102.8512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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